Abstract: This paper considers an aeroelastic two-dimensional wing-flap system with uncertainty and external disturbance. Nonlinear stiffness in pitch is expressed as the second-order polynomial form. In the uncontrolled aeroelastic ...

Abstract: The aerodynamic interaction between a rotor and an obstacle results in a complex flow field that can negatively impact rotor performance and handling qualities. To address this issue, a panel–lattice Boltzmann hybrid method ...